# Service difficulty reports: Mcdonnell-Douglas DC-10-30

A list on [Mcdonnell-Douglas DC-10-30](https://openairdocs.org/model/mcdonnell-douglas-dc-10-30.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 56 · 2,776 reports

- [SDR ZTRR20200910002](https://openairdocs.org/sdr/ZTRR20200910002.md): Hinge · departed · Aug 30, 2020 · N612AX · Doug DC1030 · Nacelle/Pylon, Main Frame
  > 2020-08-30 UPON LANDING DURING MX WALK-AROUND NR 2 ENGINE RIGHT CORE COWL WAS NOTICED TO HAVE FAILED DURING FLIGHT, PI-REP ENG 2 CORE COWL DAMAGED AND PIECES MISSING. CONCLUSIVE FAILURE IS UNDETERMINED, TWO POSSIBILITIES WHICH COULD RESULT IN SUCH FAILURE ARE
- [SDR ZTRR20200708001](https://openairdocs.org/sdr/ZTRR20200708001.md): Bolt · missing · Jul 3, 2020 · N522AX · Doug DC1030 · Pneumatic Distribution System
  > "AT ROTATE SPEED NR 2 ENG INDICATED FIRE. ALL ENG INDICATORS DISPLAYED NORMAL PARAMETERS FOR CONDITIONS. PERFORMED ENG SHUTDOWN IAW QRH. UPON PLACING FUEL LEVER TO OFF, FIRE INDICATION EXTINGUISHED. SHORTLY THEREAFTER NR 2 ENG REV PSI LIGHT BEGAN TO FLICKER UN
- [SDR FDEA201311072713](https://openairdocs.org/sdr/FDEA201311072713.md): Indicator · failed · Nov 7, 2013 · N321FE · Doug DC1030 · Escape Slide
  > DOOR EVACUATION SLIDE REMOTE PRESS-TO-TEST SWITCH DOESN'T LIGHT WHEN PRESSED. REPLACED LAMP AND CHANGED BATTERIES IAW AMM 25-61-03-2, SWITCH STILL DOES NOT LIGHT WHEN PRESSED. REMOVED AND REPLACED THE R1 DOOR REMOTE SLIDE PACK PRESSURE INDICATOR IAW AMM 25-
- [SDR CA130704005](https://openairdocs.org/sdr/CA130704005.md): Windshield · cracked · Jul 3, 2013 · Doug DC1030 · Flight Compartment Windows
  > (CAN) IN FLIGHT, THE L1 WINDOW BEGAN ARCING AND THE OUTER PANE, CRAZED, CRACKED INTO MULTIPLE PIECES. THE CREW TURNED OFF THE ANTI-ICE AND THE ACFT CONTINUED TO DESTINATION. THE L1 WINDOW AND ANTI-ICE CONTROLLER WERE REPLACED AND THE ACFT RETURNED TO SERVICE.
- [SDR CA120523001](https://openairdocs.org/sdr/CA120523001.md): Cable · broken · May 19, 2012 · Doug DC1030 · Stabilizer Control System
  > (CAN) IN CRUISE CREW NOTICED THAT THE LT SIDE OF THE HORIZONTAL STABILIZER MECHANICAL CONTROL LEVERS, LT SIDE OF THE SUITCASE HANDLES. RAPIDLY MOVED TO THE NOSE DOWN POSITION. THE CREW RETURNED TO THE NEAREST SUITABLE AIRPORT. MAINTENANCE FOUND THE LT HORIZ
- [SDR CA120504010](https://openairdocs.org/sdr/CA120504010.md): Valve · malfunctioned · Apr 30, 2012 · Doug DC1030 · Engine Thrust Reverser
  > (CAN) IN CRUISE, ENGINE NR 2 REVERSER PRESSURE LIGHT ILLUMINATED IAW AOM PROCEDURE, CREW PERFORMED A PRECAUTIONARY SHUTDOWN AND RETURNED TO DEPARTING STATION. MAINTENANCE REPLACED THE OVER PRESSURE INLET SHUTOFF VALVE AND THE ACFT WAS RETURNED TO SERVICE.
- [SDR CA120504008](https://openairdocs.org/sdr/CA120504008.md): Connector · sheared · Apr 27, 2012 · Doug DC1030 · Electrical Power System Wiring
  > (CAN) IN CRUISE, CREW EXPERIENCED MULTIPLE POWER INTERRUPTIONS CAUSING, BUSS OFF. LIGHTS TO ILLUMINATE. CREW LANDED AT NEAREST SUITABLE AIRPORT WHERE MAINTENANCE DISCOVERED THE T1 TERMINAL ON THE NR 1 GENERATOR LOOSE. TERMINAL WAS RE-SECURED AND THE ACFT RET
- [SDR CA120211001](https://openairdocs.org/sdr/CA120211001.md): Blocker Door · damaged · Feb 7, 2012 · Doug DC1030 · Engine Thrust Reverser
  > (CAN) AFTER LANDING, CREW OBSERVED THE NR 3 REVERSER, UNLOCK AND PRESSURE, LIGHTS REMAINED ILLUMINATED. MAINTENANCE DISCOVERED THAT THE BLOCKER DOORS AND THE BRACKETS THAT ATTACH THE JACKSCREWS TO THE SLIDING PANEL HAD BECOME DAMAGED/BROKEN POSSIBLY DUE TO O
- [SDR CNMA20110034](https://openairdocs.org/sdr/CNMA20110034.md): Engine · failed · Aug 8, 2011 · N603AX · Doug DC1030 · Engine (Turbine/Turboprop)
  > 2000 FT FROM LEVEL OFF NR1 ENGINE SHUTDOWN, EGT RED FLAG WITH NO N1 OR N2. PREFORMED QRH PROCEEDURE. METAL IN TAILPIPE & EXCESSIVE DAMAGE TO LPT. R & R NR1 ENG IAW WC 10UN-101. ACHIEVED ENG PARAMETERS IAW MM 71-00.
- [SDR CNMA20110032](https://openairdocs.org/sdr/CNMA20110032.md): Drive Assy · sheared · Jun 11, 2011 · N531AX · Doug DC1030 · Stabilizer Control System
  > A/P OUT OF TRIM LT CAME ON INTERMITTENTLY DURING FLT. STAYED ON FOR 30 SEC TO 3 MTS. NO PITCH TRIM CHANGE DURING ILLUMINATION. TURNED OFF AP & ACFT IN TRIM DURING DESCENT. ACFT DECENDED THROUGH SET ALT TURNED OFF AP & NOTICED ACFT WAS VERY OUT OF TRIM, IN
- [SDR CNMA20110029](https://openairdocs.org/sdr/CNMA20110029.md): Oven · burned · May 26, 2011 · N531AX · Doug DC1030 · Buffet/Galleys
  > AFT GALLEY OVEN FIRE. INSIDE OF 2-21. FOLLOWED QRH PROCEDURES. CONTINUED (ALL OVENS NEED TO BE CLEANED) R & R OVEN IAW 25-30 CLEANED ALL OTHER OVENS. NO EXCESS DRIPPINGS OR CRUMBS.
- [SDR CNMA20110026](https://openairdocs.org/sdr/CNMA20110026.md): Connector · damaged · May 6, 2011 · N270AX · Doug DC1030 · Fire Protection System Wiring
  > NR 2 ENGINE FIRE INDICATION ILLUMINATED (LOOP A ONLY W/ ALL ASSOC WARNINGS - LOOP B WAS DEFERRED) PERFORMED ENGINE FIRE CL (QRH 4-1-1-1) NR 1 FIRE BOTTLE FIRED AND FIRE INDICATION WENT OUT W/ IN 30 SECONDS IAW CL. PERFORMED RECOMMENDED FIRE WARNNING TEST, TES
- [SDR CNMA20110024](https://openairdocs.org/sdr/CNMA20110024.md): Light · no test · May 2, 2011 · N522AX · Doug DC1030 · Escape Slide
  > L1 DOOR SLIDE EMERGENCY LIGHTS FAILED TO ILLUMINATE DURING OPS TEST. SLIDE DEPLOYED NORMALLY. REPLACED SLIDE ASSY.
- [SDR CNMA20110010](https://openairdocs.org/sdr/CNMA20110010.md): Coalescer Bag · odor · Apr 11, 2011 · N720AX · Doug DC1030 · Humidity Control System
  > OILY BURNING ODOR THROUGHOUT CABIN AND FLIGHT DECK. AFTER REPLACEMENT OF NR 1 PACK & COALESER BAGS, RAN ENGINES AT MPA ONE AT A TIME & ISOLATED PNEUMATICS, NO OBVIOUS ODOR ON FLT DECK, CABIN OR LOWER GALLEY AREA.
- [SDR CNMA20110007](https://openairdocs.org/sdr/CNMA20110007.md): Pan · corroded · Mar 24, 2011 · N612AX · Doug DC1030 · Fuselage Miscellaneous Structure
  > FWD P17, STA 870, LWR BILGE LAV DUMP PAN HAS SEVERAL AREAS OF CORROSION ON TOP AND RT SIDE OF PAN. REMOVED CORROSION FROM RT SIDE OF PAN FOUND TO BE WITHIN LIMITS IAW SRM VOL 1 53-00-01, FIG 1A, PG 6. REPLACED TOP PANEL IAW SRM VOL I 51-31-01 PG 1 AND REPL
- [SDR CNMA20110011](https://openairdocs.org/sdr/CNMA20110011.md): Intercostal · corroded · Mar 19, 2011 · N612AX · Doug DC1030 · Fuselage Miscellaneous Structure
  > SUPPORT ANGLE AND INTERCOSTAL AT APPROX LONGERON 44L HAS AREAS OF CORROSION AND FASTENER HEADS POPPED FROM STA 535 TO 595. REPAIRED INTERCOSTAL IAW SRM VOL I 53-00-01, FIG 8, PG 27. REMOVED CORR IAW SRM VOL II 51-21-01, PG 28 AND REMOVED BAD FASTNER IAW SRM V
- [SDR CNMA20110006](https://openairdocs.org/sdr/CNMA20110006.md): Attach Angle · corroded · Mar 19, 2011 · N612AX · Doug DC1030 · Fuselage Main, Attach Fittings
  > CORROSSION ON FUSELAGE FRAME ATTACH ANGLE AT LONGERON 51L STA. 1119. REMOVED CORROSSION FOUND OUT OF LIMITS FABRICATED REPAIR DOUBLER FROM.080 7075-0 HEAT TREATED TO T6 IAW SRM VOL I 53-30-00, FIG 8, PG 31.
- [SDR CNMA20110005](https://openairdocs.org/sdr/CNMA20110005.md): Door Frame · corroded · Mar 19, 2011 · N612AX · Doug DC1030 · Fuselage Main, Structure
  > SURFACE CORROSSION ON AFT PIT DOOR FWD SIDE OF FRAME ON LOWER AFT SIDE AT LONGERON 42L TO 46L AT STA 1957. R & R FRAME AT STA 1957 IAW SRM VOL II 51-35-01, PG 1 AND 51-33-01, PG 34.
- [SDR CNMA20110004](https://openairdocs.org/sdr/CNMA20110004.md): Bulkhead · cracked · Mar 19, 2011 · N612AX · Doug DC1030 · Nacelle/Pylon, Bulkhead/Firewall
  > NR 3 PYLON HAS CRACK ON AFT BULKHEAD UPPER INBD FLANGE COMING OUT OF RADIUS AT PYLON STA 418. REMOVED NR 3 PYLON REPLACED AFT PYLON BULKHEAD IAW DWG NR AWB70125 RE-INSTALLED PYLON IAW MM 54-00-01 LEAK AND OPS CHECK GOOD.
- [SDR CA110209015](https://openairdocs.org/sdr/CA110209015.md): Sensor · misrigged · Feb 7, 2011 · Doug DC1030 · Landing Gear Retraction/Extension System
  > AFTER DEPARTURE THE LANDING GEAR WOULD NOT RETRACT NORMALLY, HAD TO USE THE OVERRIDE. LANDING GEAR ANTI-RETRACTION PUSH/PULL CABLES ADJUSTED IAW AMM 32-31-01 AND LANDING GEAR GND SENSE CONTROL MECH ADJUATED IAW AMM 32-24-01. LANDING GEAR GND SENSE CONTROL ADJ
- [SDR CNMA20110002](https://openairdocs.org/sdr/CNMA20110002.md): Engine · failed · Feb 7, 2011 · N531AX · Doug DC1030 · Engine (Turbine/Turboprop)
  > NR 2 ENG SHUTDOWN DURING CLIMB ACCOMPLISHED QRH PROCEDURE. REPLACED NR 2 ENGINE PER CARD 10UN-201 OPS CHECK NORMAL LEAK CHECKED OK POWER ASSURANCE OK.
- [SDR CNMA20110001](https://openairdocs.org/sdr/CNMA20110001.md): Mec · defective · Feb 6, 2011 · N621AX · Doug DC1030 · Fuel Control/Turbine Engines
  > AFTER 1+ 25 INTO FLT. NOTICED NR 3 ENG N 2 FLUX BETWEEN 95-87 PERCENT N 2 ALSO NOTICE CONSIDERABLE VIBRATION NR 3 FUEL LEVER. AFTER NR 3 THROTTLE TO IDLE NOTICED NR 3 ENG FF/ EGT/ N2 ALSO FLUX. PERFORMED ENG FAILURE/ SHUTDOWN IN FLT. CKLIST IAW QRH 4-1-2-7.
- [SDR CNMA20100036](https://openairdocs.org/sdr/CNMA20100036.md): Scavenge Pump · leaking · Dec 29, 2010 · N522AX · Doug DC1030 · Turbine Engine Oil System
  > NR 3 ENG OIL QTY WENT TO ZERO IN FLIGHT, VERIFIED BY LOSS OF OIL PRESS & LOW OIL PRESS LIGHT. TROUBLESHOT DOWN TO NR 3 ENGINE OIL LUBE AND SCAVENGE PUMP ASSY. R & R PUMP ASSY IAW MM 79-20-04, SERVICED 25 QTS OF OIL IN ENGINE LEAK CKS AND OPS CKS GOOD.
- [SDR CNMA20100035](https://openairdocs.org/sdr/CNMA20100035.md): Strainer · clogged · Dec 29, 2010 · N612AX · Doug DC1030 · Turbine Engine Oil System
  > ENG 3 OIL STRAINER CLOG LIGHT ILLUMINATED STEADY IN FLIGHT, ACCOMPLISHED QRH PROCEDURE NR3 ENGINE SHUTDOWN. C/A: REPLACED ENGINE.
- [SDR CNMA20100034](https://openairdocs.org/sdr/CNMA20100034.md): Smoke Detector · false activation · Nov 28, 2010 · N270AX · Doug DC1030 · Smoke Detection
  > ONE SMOKE DETECTOR LIGHT ON AND APPLICABLE CARGO FIRE LIGHT ON (FWD CARGO FIRE LIGHT ON DISCHARGED FIRE BOTTLES). REPLACED FWD CARGO NR3 SMOKE DETECTOR IAW AMN 26-14 AND TESTED GOOD. REPLACED AUX MWACS (MASTER WARNING CONTROL UNIT) IAW AMM 33-15 REPLACED TEST
- [SDR CNMA20100032](https://openairdocs.org/sdr/CNMA20100032.md): Support Fitting · corroded · Nov 4, 2010 · N270AX · Doug DC1030 · Fuselage, Landing Gear Attach Fittings
  > CTR LANDING GEAR LT AND RT TRUNNION SUPPORT FITTING CORRODED ON TOP AROUND BOLT HOLES. CLEANED CORROSION IAW EO 5310E0973 ROTARY PEEN REWORK AREA IAW DPS 4.999-2. PERFORMED HFEC INSP IAW NDT MANUAL, PART 6 TO VERIFIY NO CORROSION REMAINS. REPLACED HARDWARE WI
- [SDR WRLA20100810431](https://openairdocs.org/sdr/WRLA20100810431.md): Slide Raft · deployed · Aug 10, 2010 · N136WA · Doug DC1030 · Escape Slide
  > L 1 DOOR SLIDE WAS FOUND TO BE PARTIALLY DEPLOYED WHILE STILL ATTACHED TO THE DOOR. THE GIRT BAR WAS NOT ENGAGED. THE DOOR ASSIST BOTTLE WAS FULL. THE SLIDE/RAFT BOTTLE WAS FULLY DISCHARGED. THE SLIDE SHROUD WAS DAMAGED. NO EVIDENCE OF DAMAGE TO THE DOOR
- [SDR CNMA20100028](https://openairdocs.org/sdr/CNMA20100028.md): Panel · corroded · Jul 24, 2010 · N522AX · Doug DC1030 · Wing, Plate/Skin
  > EXFOLIATED CORROSION ON RT WING LOWER PLATE BELOW ACCESS PANEL 616BB AT XQRS 346. REMOVED DAMAGED SECTION OF LOWER WING SKIN, ACCOMPLISHED SURFACE SCAN AND OPEN HOLE HFEC INSP, ROTO PEENED AFFECTED AREA. FABRICATED ALL REPAIR PARTS. INSTALLED ALL REPAIR PARTS
- [SDR CNMA20100027](https://openairdocs.org/sdr/CNMA20100027.md): Control Handle · malfunctioned · Jul 2, 2010 · N720AX · Doug DC1030 · Landing Gear Selector
  > LANDING GEAR HANDLE WOULD NOT COME UP. FOLLOWED QRH PROCEDURE, RETURNED TO DEPARTURE. JACK ACFT IAW MM-07-11, PERFORM EXTENSION & RETRACTION OF ALL MLG'S. OPS CKS NORMAL AIW MM 32-30 DOWN JACK ACFT IAW MM 07-11.
- [SDR WRLA20100621395](https://openairdocs.org/sdr/WRLA20100621395.md): Web · cracked · Jun 21, 2010 · N137WA · Doug DC1030 · Nacelle/Pylon Miscellaneous Structure
  > WHILE IN ATL DURING A-5 CHECK A SPECIAL INSPECTION (SI) WAS PERFORMED ON THE NR 3 PYLON AND THE UPPER WEB WAS FOUND CRACKED AT THE CORNER OF THE GENERATOR FEEDER CABLE PASS THROUGH CUTOUT LOCATED AT YUS 338. FOUND BY ATLANTA INSPECTOR. PERMANENT REPAIR MADE
- [SDR CNMA20100026](https://openairdocs.org/sdr/CNMA20100026.md): Slide · defective · Jun 2, 2010 · N270AX · Doug DC1030 · Escape Slide
  > DOOR 3L EVACUATION SLIDE REMOTE PRESURE PRESS TO TEST INDICATOR LIGHT STAYS ON CONTINUOUSLY. REPLACED L-3 DOOR SLIDE ASSY - OPS CHECK NORMAL. OK FOR SERVICE. M/M REF. 25-61.
- [SDR CNMA20100024](https://openairdocs.org/sdr/CNMA20100024.md): Duct · blown · May 14, 2010 · N603AX · Doug DC1030 · Engine Cooling System
  > NR 1 ENGINE FIRE WARNING DURING CLIMB OUT AT 13000 FT. N1'S 103.5. FIRE WARNING EXTINGUISHED WHEN THROTTLE WAS RETARDED. COMPLIED WITH QRH 4-1-1-1. INSP NR 1 ENG FOUND BLOWN DUCT FOR HP RECOUP AIR ASSY. REPLACED NR 1 ENG HP RECOUP AIR ASSY DUCT WITH SERVIC
- [SDR CNMA20100019](https://openairdocs.org/sdr/CNMA20100019.md): Decoder · failed · May 8, 2010 · N612AX · Doug DC1030 · Entertainment System
  > F/A'S BROUGHT TO ATTENTION OF COCKPIT THAT IF READING LIGHTS, CALL LIGHTS AND AUDIO INOP IN B ZONE MAY EFFECT O2 GENERATORS, MAINT CONTROL CONFIRMED RETURNED TO DEPARTURE. R&R SECTION TIMER DECODER IN ZONE "B", OTBD IAW AMM 23-33 CHK OPS NORMAL. ACCOMPLISHE
- [SDR CNMA20100020](https://openairdocs.org/sdr/CNMA20100020.md): Floor Support · corroded · May 6, 2010 · N621AX · Doug DC1030 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR PANEL SUPPORT BS 485-515 RBL 55-60. DAMAGED FLOOR SUPPORT WAS REMOVED. NEW FLOOR SUPPORT PN OAI-53-0002 WAS FABRICATED AND INSTALLED USING FASTENERS BOCR1SCEGDG B/N 517060 B/N 828982 IAW SRM VOL 2, 51-35-01, PAGE 1 AND 51-33-01 PAGE 34 B1CB
- [SDR 22AA201000068](https://openairdocs.org/sdr/22AA201000068.md): Stud · damaged · Apr 25, 2010 · N524MD · Doug DC1030 · Engine (Turbine/Turboprop)
  > OIL PRESSURE NR 2 GAUGE DROPPED TO ZERO AND NR 2 OIL PRESS LOW LIGHT CAME ON, ENGINE SHUTDOWN IAW CHECK LIST. FOUND OIL LEAK COMING FROM CRANK PAD COVER, INSTALLED 1EA COVER PAD STUD, REINSTALLED 1EA COVER PAD STUD IAW GE SPM 70-48-01, REINSTALLED COVER PAD IA
- [SDR WRLA20100422353](https://openairdocs.org/sdr/WRLA20100422353.md): Fitting · corroded · Apr 22, 2010 · N136WA · Doug DC1030 · Fuselage, Landing Gear Attach Fittings
  > REF DELTA N/R 93 CENTER LINE LANDING GEAR LT ATTACH FITTING CENTER BORE PITTED IN FITTING. REWORK CTR LANDING GEAR LT TRUNNION FITTING IAW DELTA ERA 481717-14.
- [SDR CNMA20100023](https://openairdocs.org/sdr/CNMA20100023.md): Intercostal · damaged · Apr 11, 2010 · N621AX · Doug DC1030 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL BS 1900-1921 STR 43R. DAMAGED INTERCOSTAL AND ADJACENT ANGLE WERE REMOVED. NEW INTERCOSTAL AND ANGLE PN OAI53-004/005 WERE FABRICATED AND INSTALLED IAW ES0 53-03 AND DWC VCA7012 USING FASTENERS BACRI5CE606 B/N 5828382 AND BACR30MY6X3
- [SDR CNMA20100022](https://openairdocs.org/sdr/CNMA20100022.md): Angle · corroded · Apr 11, 2010 · N621AX · Doug DC1030 · Fuselage Miscellaneous Structure
  > CORROSION ON NUT PLATE ANGLE BS 1099 LBL 41. REMOVED ANGLE AND NEW PN AOA7GG7-23 INSTALLED WITH NEW ANCHOR NUTS AND RIVETS IAW SRM VOL 2 51-31-01. PN BACB30NWGK3 B/N 5836738.
- [SDR CNMA20100021](https://openairdocs.org/sdr/CNMA20100021.md): Angle · corroded · Apr 7, 2010 · N621AX · Doug DC1030 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE C/T AFT CARGO TANK WALL BS 1781 4 PLACES RBL 30, RBL 36, LBL 30, LBL 36. DAMAGED ANGLE REMOVED, NEW FABRICATED PN OAI-53-00-11 IAW DWG AFA7548-21 & GMM 4.45 AND INSTALLED WITH FASTNERS IAW SRM VOL 2 51-31-01.
- [SDR 22AA201000067](https://openairdocs.org/sdr/22AA201000067.md): Receptacle · loose · Apr 5, 2010 · N526MD · Doug DC1030 · Cargo/Baggage Doors
  > PASSING FL 8000 AFT CARGO DOOR A & B LIGHT ILLUMINATED INTERMITTENT UNABLE TO PRESSURIZE, RETURN TO DEPARTURE. TROUBLE SHOOTING FOUND LOOSE CONNECTOR ON LATCH DOOR ACTUATOR IAW MM 52-33-02 AND OPS CHECKED GOOD IAW MM 52-33-00.
- [SDR CNMA20100018](https://openairdocs.org/sdr/CNMA20100018.md): Floorbeam · corroded · Apr 1, 2010 · N621AX · Doug DC1030 · Fuselage Main, Floor Beam
  > BS 2007, LBL 20-28 CORROSION ON M/D FLOOR SUPPORT TEE CHORD. ALL OPEN HOLES WERE NDT INSPECTED - NO CRACKS OR CORROSION WERE FOUND. THIS SECTION OF CHORD WAS INCLUDED IN THE REPAIR OF NRC -387. SEE NRC 387. (NONRO 387 CORRODED SECTION OF CHORD WAS TRIMMED OU
- [SDR CNMA20100017](https://openairdocs.org/sdr/CNMA20100017.md): Floorbeam · corroded · Apr 1, 2010 · N621AX · Doug DC1030 · Fuselage Main, Floor Beam
  > BS 2007, LBL 53-68 CORROSION ON FLOOR SUPPORT TEE CHORD. ALL OPEN HOLES NDT INSPECTED - NO CRACKS OR CORROSION FOUND. THIS SECTION WAS INCLUDED IN THE REPAIR OF NRC 387. NRC 387. (NONRO 387, CORRODED SECTION OF CHORD WAS TRIMMED OUT. NEW SECTION FABRICATED FR
- [SDR CNMA20100016](https://openairdocs.org/sdr/CNMA20100016.md): Floorbeam · corroded · Apr 1, 2010 · N621AX · Doug DC1030 · Fuselage Main, Floor Beam
  > BS 2007 LBL 77 CORROSION ON TEE CHORD FLOOR SUPPORT. ALL OPEN HOLES WERE NDT INSPECTED - NO CRACKS OR CORROSION FOUND. THIS SECTION OF CHORD WAS INCLUDED IN THE REPAIR OF NRC-387. SEE NRC 387. (NONRO 387, CORRODED SECTION OF CHORD WAS TRIMMED OUT. NEW SECTI
- [SDR CNMA20100015](https://openairdocs.org/sdr/CNMA20100015.md): Floorbeam · corroded · Apr 1, 2010 · N621AX · Doug DC1030 · Fuselage Main, Floor Beam
  > BS 2007, LBL16 CORROSION ON THE TEE CHORD FLOOR STRUCTURE. CORRODED SECTION OF CHORD WAS TRIMMED OUT. NEW SECTION FABRICATED FROM THE TEE PN NJC6040-175 WAS INSTALLED WITH SPLICES PN N621AX-NRC387-1/-2 IAW SRM VOL I 53-40-00, FIG 16 AND USING FASTENERS IAW S
- [SDR CNMA20100014](https://openairdocs.org/sdr/CNMA20100014.md): Floor Support · corroded · Mar 28, 2010 · N621AX · Doug DC1030 · Fuselage Miscellaneous Structure
  > CORROSION ON CTR CARGO LWR PANEL SUPPORT BS 1700-1781 BL-0.3, DAMAGED AREAS TRIMMED OUT. AREAS REINFORCED WITH DOUBLERS PN N621AX-NRC361-1 (QTY X3) FABRICATED AND INSTALLED IAW SRM VOL 1 53-00-01, FIG 8 USING FASTENERS IAW SRM VOL 2, 51-35-01, PAGE 1.
- [SDR CNMA20100013](https://openairdocs.org/sdr/CNMA20100013.md): Floorbeam · corroded · Mar 28, 2010 · N621AX · Doug DC1030 · Fuselage Main, Floor Beam
  > CORROSION ON CTR CARGO LWR PANEL SUPPORT BS 1741 LBL 16. DAMAGED SUPPORT REMOVED NEW FABRICATED PN OAI-53-0008 IAW SRM DWG AD0145-30 & OMNI GMM 4.45 AND INSTALLED WITH FASTNERS IAW SRM VOL 2 51-35-01, PAGE 1.
- [SDR CNMA20100012](https://openairdocs.org/sdr/CNMA20100012.md): Floorbeam · corroded · Mar 28, 2010 · N621AX · Doug DC1030 · Fuselage Main, Floor Beam
  > CORROSION ON CTR CARGO LWR PANEL SUPPORT BS 1741 RBL 16. DAMAGED SUPPORT REMOVED NEW FABRICATED PN OAI-53-0007 IAW SRM DWG AD00145 OMNI GMM 4.45 AND INSTALLED WITH FASTNERS IAW SRM VOL 2 51-35-01, PAGE 1.
- [SDR CNMA20100011](https://openairdocs.org/sdr/CNMA20100011.md): Floorbeam · corroded · Mar 28, 2010 · N621AX · Doug DC1030 · Fuselage Main, Floor Beam
  > CORROSION ON CTR CARGO LWR PANEL SUPPORT BS 1741 RBL 12-14. DAMAGED SUPPORT REMOVED NEW FABRICATED PN OAI-53-0009 IAW DWG AD00145 & OMNI GMM 4-45 AND INSTALLED WITH FASTNERS IAW SRM VOL 2 51-35-01, PAGE 1.
- [SDR 22AA201000067A](https://openairdocs.org/sdr/22AA201000067A.md): Control Cable · broken · Mar 28, 2010 · N524MD · Doug DC1030 · Aileron Control System
  > ACFT ROLLS WHEN SPEED BRAKE IS EXTENDED. DIFFERENCE SHOWS ON SPI. DURING INSP FOUND RT/LT INBD AILERONS OUT OF RIGGING. ALSO ON PRE/FLT FOUND LT WING GROUND SPOILERS NOT DEPLOYING FULLY & SPOILER HANDLE NOT RETRACTING AUTOMATICALLY. ALSO SPOILER PANEL 1 & 2 NO
- [SDR CNMA20100005](https://openairdocs.org/sdr/CNMA20100005.md): Fan · shorted · Mar 12, 2010 · N810AX · Doug DC1030 · Air Distribution Fan
  > AFTER T/O, BURNED SMELL FROM "A" ZONE WAS NOTICED. CABIN AIR RECIRC FAN NR1 SW WAS TRIPPED, BUT FAN NR15 WAS STILL THERE IN AFT "A" ZONE, SO ALL RECIRC FANS TURNED OFF (OK AFTER THAT). R & R WITH NEW FAN IAW 21-22-10. OPS CHECK GOOD.

Next page: https://openairdocs.org/model/mcdonnell-douglas-dc-10-30/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE aircraft_model_key = 'DC1030'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/mcdonnell-douglas-dc-10-30/reports

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